Direct numerical simulation of round supersonic free jet

被引：0
|
作者：
Li, XL [1 ]
Fu, DX [1 ]
Ma, YW [1 ]
机构：
[1] Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China
来源：
RECENT ADVANCES IN FLUID MECHANICS | 2004年
关键词：
group velocity control; direct numerical simulation; jet;
D O I：
暂无
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
6th order group-velocity control scheme is constructed and used in direct numerical simulation of the round supersonic free jet. The exit Mach number of the jet is 2.5. The disturbance waves generated by the jet are showed and the reason of the existence up-stream propagated wave is analyzed.
引用
收藏
页码：735 / 738
页数：4
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